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导弹末敏弹控制系统的设计与仿真
引用本文:王建军,刘荣忠,张宇.导弹末敏弹控制系统的设计与仿真[J].系统仿真学报,2007,19(8):1876-1878.
作者姓名:王建军  刘荣忠  张宇
作者单位:1. 山东理工大学机械工程学院测控技术与仪器系,山东淄博,255049
2. 南京理工大学机械工程学院202教研室,江苏南京,210094
基金项目:国家自然科学基金;山东省自然科学基金
摘    要:通过研究导弹末敏弹的控制过程,设计了控制系统的硬件部分,重点建立了导弹的控制系统模型,并利用MATLAB对导弹控制系统进行了校正和仿真,获得了相应的校正参数,仿真结果证明所设计的控制系统合乎技术和设计性能要求。

关 键 词:控制系统  仿真  计算机控制  导弹  建模  校正
文章编号:1004-731X(2007)08-1876-03
收稿时间:2006-03-10
修稿时间:2006-05-25

Control System Design and Simulation of Guided Missile with Terminal Sensitive Bullets
WANG Jian-jun,LIU Rong-zhong,ZHANG Yu.Control System Design and Simulation of Guided Missile with Terminal Sensitive Bullets[J].Journal of System Simulation,2007,19(8):1876-1878.
Authors:WANG Jian-jun  LIU Rong-zhong  ZHANG Yu
Institution:1.School of Mechanical Engineering, Shandong University of Technology, Zibo 255049, China; 2.School of Mechanical Engineering, Nanjing University of science and Technology, Nanjing 210094, China
Abstract:Through studying the control process of guided missile with terminal sensitive bullets, the hardware of the control was designed, and the control system model of the guided missile was established. Using the MATLAB software tool, the control system was revised and simulated, and the revised PID parameters were acquired. The simulating results prove that the performances of the control system model with the revised parameters are fit for the designing demand.
Keywords:MATLAB  PID
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